CN104046822B - A method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening - Google Patents

A method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening Download PDF

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CN104046822B
CN104046822B CN201410320272.XA CN201410320272A CN104046822B CN 104046822 B CN104046822 B CN 104046822B CN 201410320272 A CN201410320272 A CN 201410320272A CN 104046822 B CN104046822 B CN 104046822B
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tantalum
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张于胜
张小明
牛红志
卢金文
白新房
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Northwest Institute for Non Ferrous Metal Research
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Abstract

The invention discloses the method that a kind of solution strengthening preparation has the tantalum-base alloy of gradient-structure, the method is: one, tantalum powder is placed in nitriding furnace, carries out cxygen nitrogen coinfiltration process to tantalum powder; Two, the tantalum powder after cxygen nitrogen coinfiltration process is placed in plasma agglomeration stove, sintering processes is carried out to the tantalum powder after cxygen nitrogen coinfiltration process, obtains tantalum-base alloy; Three, tantalum-base alloy is placed in vacuum annealing furnace, vacuum annealing process is carried out to tantalum-base alloy.Method of the present invention is first by carrying out cxygen nitrogen coinfiltration process to tantalum powder, make oxygen nitrogen in tantalum powder from top layer to core distribution gradient, then tantalum-base alloy is formed by sintering processes, the hardness of tantalum-base alloy is also from top layer to core distribution gradient, finally by vacuum annealing process, the oxygen nitrogen in tantalum-base alloy is spread gradually to core from border, can in a big way the mechanical property of controlled material, realize the intensity of tantalum-base alloy and the good combination of plasticity, extend the work-ing life of material.

Description

一种固溶强化制备具有梯度结构的钽基合金的方法A method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening

技术领域technical field

本发明属于高强钽合金的制备技术领域,具体涉及一种固溶强化制备具有梯度结构的钽基合金的方法。The invention belongs to the technical field of preparation of high-strength tantalum alloys, and in particular relates to a method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening.

背景技术Background technique

难熔金属钽和铌用途极广,但与其熔点相比,其潜在的强度性能远未发掘出来,不能满足人们越来越高的应用需求。即使在低的工作温度下,也会由于其强度不足,导致其疲劳、磨损和腐蚀等性能的降低,从而缩短零构件的使用寿命。目前国内外普遍采用钽或钽合金替代金铂合金制作化纤湿法或干湿法纺丝用的喷丝头,但其耐磨性较差,易划伤,导致在一定压力下长时间工作易发生变形,从而增加生产成本,影响喷丝头的纺丝效果,导致疵点、毛丝降等率偏高。因此,提高钽合金的强度性能对满足特殊工艺的生产具有重要的意义。The refractory metals tantalum and niobium are extremely versatile, but compared with their melting points, their potential strength properties are far from being discovered, and they cannot meet people's increasing application requirements. Even at low working temperature, due to its insufficient strength, it will reduce its fatigue, wear and corrosion performance, thereby shortening the service life of components. At present, tantalum or tantalum alloys are commonly used instead of gold-platinum alloys at home and abroad to make spinnerets for chemical fiber wet or dry-wet spinning, but their wear resistance is poor and they are easy to scratch, which makes it easy to work under a certain pressure for a long time. Deformation occurs, thereby increasing production costs, affecting the spinning effect of the spinneret, resulting in high defects and high yarn degradation rates. Therefore, improving the strength properties of tantalum alloys is of great significance to meet the production of special processes.

目前钽合金主要的强化方法是固溶强化和析出强化。例如在航天和导弹技术中应用多年的Ta-7.5W、Ta-12W、Ta-15W系列合金,是依赖于钨的固溶强化,其强度随钨含量的增加而提高,但钽钨系列合金的加工难度较大。另外,在钽钨合金的基础上加入了铪和碳等元素,通过钨和铪的固溶强化及碳化铪的析出相强化可以进一步提高强度性能,但其仅达到800MPa左右。多元钽合金的成分比较复杂,且添加的钨和铪等元素的价格比较昂贵,合金的加工性能较差。因此,低成本高强钽合金的开发和研究不仅可以有效的节约材料的用量,而且还可以扩大钽合金的应用范围。At present, the main strengthening methods of tantalum alloys are solid solution strengthening and precipitation strengthening. For example, Ta-7.5W, Ta-12W, and Ta-15W series alloys, which have been used in aerospace and missile technology for many years, rely on the solid solution strengthening of tungsten, and their strength increases with the increase of tungsten content, but the tantalum-tungsten series alloys Processing is more difficult. In addition, elements such as hafnium and carbon are added to the tantalum-tungsten alloy, and the strength performance can be further improved through the solid solution strengthening of tungsten and hafnium and the precipitation phase strengthening of hafnium carbide, but it only reaches about 800MPa. The composition of the multi-component tantalum alloy is relatively complex, and the price of the added elements such as tungsten and hafnium is relatively expensive, and the processing performance of the alloy is poor. Therefore, the development and research of low-cost high-strength tantalum alloys can not only effectively save the amount of materials used, but also expand the application range of tantalum alloys.

一般情况下,钽中固溶的氧和氮是作为损害塑韧性的有害元素,在钽及钽合金的加工制备过程中尽力减少。如果利用氮对钽的固溶强化作用,同时最大限度保留其塑性就可以很好的解决这一技术难题,但是目前有关高氧氮钽基合金的相关研究基本属于空白。In general, the solid solution of oxygen and nitrogen in tantalum are harmful elements that damage the plasticity and toughness, and should be minimized during the processing and preparation of tantalum and tantalum alloys. If the solid-solution strengthening effect of nitrogen on tantalum is used, this technical problem can be well solved while retaining its plasticity to the maximum extent. However, the current research on high-oxygen-nitrogen tantalum-based alloys is basically blank.

发明内容Contents of the invention

本发明所要解决的技术问题在于针对上述现有技术中的不足,提供一种固溶强化制备具有梯度结构的钽基合金的方法。该方法首先通过对钽粉末进行氧氮共渗处理,使氧氮在钽粉末中从表层到芯部呈梯度分布,然后通过烧结处理形成钽基合金,由于等离子烧结温度较低,氧氮在其中仍然呈梯度分布,使得钽基合金的硬度也从表层到芯部呈梯度分布,最后通过真空退火处理使钽基合金中的氧氮逐渐从边界向芯部扩散,能够在较大范围内调控材料的力学性能,实现钽基合金的强度与塑性的良好配合,延长材料的使用寿命。The technical problem to be solved by the present invention is to provide a method for preparing a tantalum-based alloy with a gradient structure by solid solution strengthening in view of the above-mentioned deficiencies in the prior art. In this method, the tantalum powder is first subjected to oxygen and nitrogen co-infiltration treatment, so that the oxygen and nitrogen in the tantalum powder are distributed in a gradient from the surface layer to the core, and then the tantalum-based alloy is formed through sintering treatment. Due to the low plasma sintering temperature, oxygen and nitrogen are in it It is still distributed in a gradient, so that the hardness of the tantalum-based alloy is also distributed in a gradient from the surface to the core. Finally, the oxygen and nitrogen in the tantalum-based alloy are gradually diffused from the boundary to the core through vacuum annealing, which can control the material in a wide range. The mechanical properties of the tantalum-based alloy are well matched with the strength and plasticity, and the service life of the material is extended.

为解决上述技术问题,本发明采用的技术方案是:一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,该方法包括以下步骤:In order to solve the above-mentioned technical problems, the technical solution adopted in the present invention is: a method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening, which is characterized in that the method includes the following steps:

步骤一、将钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.05m3/h~0.2m3/h,在600℃~1000℃条件下对钽粉末进行氧氮共渗处理5min~90min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目,所述氧氮共渗处理过程中控制渗氮炉中氧的体积含量不低于5%;Step 1. Put the tantalum powder in the nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.05m 3 /h~0.2m 3 /h, and carry out oxynitriding treatment on the tantalum powder under the condition of 600℃~1000℃ 5min to 90min; the mass purity of the tantalum powder is not less than 99.5%, the particle size of the tantalum powder is not less than 200 mesh, and the volume content of oxygen in the nitriding furnace is controlled to be not less than 5% during the oxynitriding process ;

步骤二、将步骤一中经氧氮共渗处理后的钽粉末置于等离子烧结炉中,调节等离子烧结炉的压强为200MPa~500MPa,在800℃~1100℃条件下将经氧氮共渗处理后的钽粉末烧结处理1min~30min,得到钽基合金;Step 2. Put the tantalum powder treated by oxynitriding in step 1 in a plasma sintering furnace, adjust the pressure of the plasma sintering furnace to 200MPa~500MPa, and put the tantalum powder treated by oxynitriding in step 1 to 200MPa~500MPa. The final tantalum powder is sintered for 1 to 30 minutes to obtain a tantalum-based alloy;

步骤三、将步骤二中所述钽基合金置于真空退火炉中,调节真空退火炉的真空度为10-1Pa~10-4Pa,在700℃~1050℃条件下将钽基合金真空退火处理0.5h~5h。Step 3. Place the tantalum-based alloy described in step 2 in a vacuum annealing furnace, adjust the vacuum degree of the vacuum annealing furnace to 10 -1 Pa to 10 -4 Pa, and vacuum the tantalum-based alloy at 700°C to 1050°C Annealing treatment 0.5h ~ 5h.

上述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,步骤一中所述氮气流量为0.08m3/h~0.12m3/h,氧氮共渗处理的温度为800℃~1000℃,氧氮共渗处理的时间为5min~30min。The above-mentioned method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening is characterized in that the flow rate of nitrogen gas in step 1 is 0.08m 3 /h to 0.12m 3 / h, and the temperature of oxynitriding treatment is 800℃~1000℃, the time of oxynitriding treatment is 5min~30min.

上述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,所述氮气流量为0.1m3/h,氧氮共渗处理的温度为900℃,氧氮共渗处理的时间为15min。The above-mentioned method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening is characterized in that the flow rate of the nitrogen gas is 0.1m 3 /h, the temperature of the oxynitriding treatment is 900°C, and the temperature of the oxynitriding treatment The time is 15 minutes.

上述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,步骤二中所述压强为200MPa~400MPa,烧结处理的温度为900℃~1000℃,烧结处理的时间为3min~10min。The above-mentioned method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening is characterized in that the pressure in step 2 is 200MPa-400MPa, the temperature of the sintering treatment is 900°C-1000°C, and the time of the sintering treatment is 3min ~10min.

上述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,所述压强为300MPa,烧结处理的温度为950℃,烧结处理的时间为5min。The above-mentioned method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening is characterized in that the pressure is 300 MPa, the sintering temperature is 950° C., and the sintering time is 5 minutes.

上述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,步骤三中所述真空度为10-1Pa~10-3Pa,真空退火处理的温度为800℃~1000℃,真空退火处理的时间为0.5h~2h。The above-mentioned method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening is characterized in that the degree of vacuum in step 3 is 10 -1 Pa to 10 -3 Pa, and the temperature of vacuum annealing is 800°C to 1000°C ℃, the time of vacuum annealing treatment is 0.5h~2h.

上述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,所述真空度为10-2Pa,真空退火处理的温度为900℃,真空退火处理的时间为1h。The above-mentioned method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening is characterized in that the degree of vacuum is 10 -2 Pa, the temperature of the vacuum annealing treatment is 900° C., and the time of the vacuum annealing treatment is 1 h.

本发明与现有技术相比具有以下优点:Compared with the prior art, the present invention has the following advantages:

1、本发明的方法首先通过对钽粉末进行表面氧氮共渗处理,使氧氮在钽粉末中从表层到芯部呈梯度分布,然后通过烧结处理形成钽基合金,由于等离子烧结温度较低,氧氮在其中仍然呈梯度分布,使得钽基合金的硬度也从表层到芯部呈梯度分布,最后通过真空退火处理使钽基合金中的氧氮逐渐从边界向芯部扩散,能够在较大范围内调控材料的力学性能,实现钽基合金的强度与塑性的良好配合,延长材料的使用寿命。1. The method of the present invention firstly carries out surface oxygen nitriding treatment on the tantalum powder, so that oxygen and nitrogen are distributed in a gradient from the surface layer to the core in the tantalum powder, and then the tantalum-based alloy is formed through sintering treatment. Due to the low plasma sintering temperature , oxygen and nitrogen are still distributed in a gradient, so that the hardness of the tantalum-based alloy is also distributed in a gradient from the surface to the core. Finally, through vacuum annealing, the oxygen and nitrogen in the tantalum-based alloy gradually diffuse from the boundary to the core, which can The mechanical properties of the material can be adjusted in a wide range to achieve a good match between the strength and plasticity of the tantalum-based alloy and prolong the service life of the material.

2、本发明的制备方法中首先通过氧氮共渗处理使氧氮含量在钽粉末中呈梯度分布,表层由固溶体或形成化合物强化,内部为软的基体,然后利用等离子低温烧结制备钽基合金,由于烧结温度相对较低,氧氮在颗粒内很难扩散均匀化,硬度仍是边界层高而芯部低呈梯度分布,所以形成了空间连续的硬软相结合的钽基合金,钽基合金具有了较高的强度,并保留了一定的塑性,最后对钽基合金进行真空退火处理,氧氮会逐渐由表层向芯部扩散,材料的力学性能随之改变。本发明的方法为传统材料赋予了优异的性能,在基础研究与工程应用方面均有十分广阔的前景。2. In the preparation method of the present invention, the oxygen and nitrogen content is distributed in a gradient in the tantalum powder through oxygen and nitriding treatment firstly, the surface layer is strengthened by a solid solution or a compound, and the interior is a soft matrix, and then the tantalum-based alloy is prepared by plasma low-temperature sintering , due to the relatively low sintering temperature, it is difficult for oxygen and nitrogen to diffuse uniformly in the particles, and the hardness is still high in the boundary layer and low in the core in a gradient distribution, so a spatially continuous tantalum-based alloy with a combination of hard and soft is formed. The alloy has high strength and retains a certain degree of plasticity. Finally, vacuum annealing is performed on the tantalum-based alloy. Oxygen and nitrogen will gradually diffuse from the surface to the core, and the mechanical properties of the material will change accordingly. The method of the invention endows traditional materials with excellent properties, and has very broad prospects in basic research and engineering applications.

3、本发明中采用氧氮共渗的固溶工艺,由于氧的催渗作用促进了氮原子在钽中的渗入,使渗层固溶的氮及形成的氮化物增加,从而增大钽中氧氮共渗的化合物层和扩散层的深度,更加有利于提高钽基合金材料的硬度及进一步改善材料的综合力学性能。3. In the present invention, the solid solution process of oxygen and nitrogen co-infiltration is adopted, because the infiltration effect of oxygen promotes the infiltration of nitrogen atoms in tantalum, so that the solid-dissolved nitrogen and nitrides formed in the infiltration layer increase, thereby increasing the tantalum. The depth of the oxynitrided compound layer and the diffusion layer is more conducive to improving the hardness of the tantalum-based alloy material and further improving the comprehensive mechanical properties of the material.

4、本发明的制备方法简单,产品致密、质量稳定且性能优异,同时重复性好。采用本发明的方法既能够得到成本较低的近净成型高强钽基合金零件,又为金属尤其是难熔金属钽、铌的强化提供了一个新的思路。同时,该方法也能够采用廉价的碳或其他元素进行粉末颗粒表面强化,为其它金属进行强化处理提供借鉴,推动金属材料强化技术的进步。4. The preparation method of the present invention is simple, the product is dense, stable in quality, excellent in performance, and good in repeatability. The method of the invention can not only obtain low-cost near-net shape high-strength tantalum-based alloy parts, but also provides a new idea for strengthening metals, especially refractory metals tantalum and niobium. At the same time, this method can also use cheap carbon or other elements to strengthen the surface of powder particles, which provides a reference for strengthening treatment of other metals and promotes the progress of metal material strengthening technology.

下面通过附图和实施例,对本发明的技术方案做进一步的详细描述。The technical solutions of the present invention will be described in further detail below with reference to the accompanying drawings and embodiments.

附图说明Description of drawings

图1为本发明实施例1制备的钽基合金的硬度压痕形貌图。Fig. 1 is a hardness indentation topography diagram of a tantalum-based alloy prepared in Example 1 of the present invention.

图2为对比例1制备的钽基合金的硬度压痕形貌图。FIG. 2 is a hardness indentation image of the tantalum-based alloy prepared in Comparative Example 1.

图3为对比例1制备的钽基合金的硬度梯度趋势图。FIG. 3 is a hardness gradient trend diagram of the tantalum-based alloy prepared in Comparative Example 1.

图4为对比例2制备的钽基合金的硬度梯度趋势图。FIG. 4 is a hardness gradient trend graph of the tantalum-based alloy prepared in Comparative Example 2.

图5为本发明实施例2制备的钽基合金的硬度压痕形貌图。Fig. 5 is a hardness indentation topography diagram of the tantalum-based alloy prepared in Example 2 of the present invention.

图6为对比例3制备的钽基合金的硬度压痕形貌图。FIG. 6 is a hardness indentation image of the tantalum-based alloy prepared in Comparative Example 3.

图7为对比例3制备的钽基合金的硬度梯度趋势图。FIG. 7 is a hardness gradient trend graph of the tantalum-based alloy prepared in Comparative Example 3.

图8为对比例4制备的钽基合金的硬度梯度趋势图。FIG. 8 is a hardness gradient trend graph of the tantalum-based alloy prepared in Comparative Example 4.

具体实施方式detailed description

实施例1Example 1

本实施例包括以下步骤:This embodiment includes the following steps:

步骤一、将400g钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.1m3/h,在900℃条件下对钽粉末进行氧氮共渗处理15min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目,所述氧氮共渗处理过程中控制渗氮炉中氧的体积含量不低于5%;Step 1. Place 400g of tantalum powder in a nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.1m 3 /h, and carry out oxynitridation treatment on the tantalum powder at 900°C for 15 minutes; the mass of the tantalum powder The purity is not less than 99.5%, the particle size of the tantalum powder is not less than 200 mesh, and the volume content of oxygen in the nitriding furnace is controlled to be not less than 5% during the oxynitriding process;

步骤二、将步骤一中经氧氮共渗处理后的钽粉末置于等离子烧结炉中,调节压强为300MPa,在950℃条件下将经氧氮共渗处理后的钽粉末烧结处理5min,得到钽基合金;Step 2. Put the tantalum powder treated by oxynitriding in step 1 in a plasma sintering furnace, adjust the pressure to 300MPa, and sinter the tantalum powder treated by oxynitriding at 950°C for 5 minutes to obtain Tantalum-based alloys;

步骤三、将步骤二中所述钽基合金置于真空退火炉中,调节真空度为10-2Pa,在900℃条件下将钽基合金真空退火处理1h。Step 3. Put the tantalum-based alloy described in step 2 in a vacuum annealing furnace, adjust the vacuum degree to 10 −2 Pa, and vacuum anneal the tantalum-based alloy at 900° C. for 1 hour.

图1为实施例1制备的钽基合金的硬度压痕形貌图;实施例1中制备的钽基合金的室温力学性能测试结果为:断裂延伸率为10.5%,具有较好的塑性,屈服强度为1500MPa(该实施例制备的钽基合金的屈服强度是纯钽粉末冶金材料屈服强度的3.95倍)。Fig. 1 is the hardness indentation topography diagram of the tantalum-based alloy prepared in Example 1; the test result of the mechanical properties at room temperature of the tantalum-based alloy prepared in Example 1 is: the elongation at break is 10.5%, has good plasticity, yields The strength is 1500MPa (the yield strength of the tantalum-based alloy prepared in this example is 3.95 times that of the pure tantalum powder metallurgy material).

对比例1Comparative example 1

对比例1与实施例1相同,其不同之处在于:不对步骤二中所述钽基合金进行真空退火处理。Comparative Example 1 is the same as Example 1, except that the tantalum-based alloy in Step 2 is not subjected to vacuum annealing.

对比例1制备的钽基合金中的氧含量为0.09%,氮含量为0.18%,钽基合金的相对密度为99%。The oxygen content in the tantalum-based alloy prepared in Comparative Example 1 was 0.09%, the nitrogen content was 0.18%, and the relative density of the tantalum-based alloy was 99%.

图2为对比例1制备的钽基合金的硬度压痕形貌图,图3为对比例1制备的钽基合金的硬度梯度趋势图,结合图2和图3可以看出,经过氧氮共渗处理和烧结处理两步工艺制备的钽基合金内部具有明显的硬度梯度结构,随着距表面距离的增加,钽基合金的微观硬度逐渐减小,从表层的7.5GPa逐渐下降到距表面距离25μm处的6.0GPa,再下降到芯部的3.2GPa。Fig. 2 is the hardness indentation topography diagram of the tantalum-based alloy prepared in Comparative Example 1, and Fig. 3 is the hardness gradient trend diagram of the tantalum-based alloy prepared in Comparative Example 1. Combining Fig. 2 and Fig. 3, it can be seen that after oxygen-nitrogen co- The tantalum-based alloy prepared by the two-step process of infiltration treatment and sintering treatment has an obvious hardness gradient structure inside. With the increase of the distance from the surface, the microhardness of the tantalum-based alloy gradually decreases, from 7.5GPa on the surface layer to the distance from the surface. 6.0GPa at 25μm, and then down to 3.2GPa at the core.

对比例1中制备的钽基合金的室温力学性能测试结果为:断裂延伸率为18%,屈服强度为1190MPa,断裂强度为1200MPa。The test results of the mechanical properties of the tantalum-based alloy prepared in Comparative Example 1 at room temperature are: the elongation at break is 18%, the yield strength is 1190 MPa, and the breaking strength is 1200 MPa.

对比例2Comparative example 2

本对比例包括以下步骤:This comparative example includes the following steps:

步骤一、将400g钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.3m3/h,常温下通入氮气1h以排出空气,然后升温至900℃,在氮气气氛下对钽粉末进行渗氮处理15min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目;Step 1. Put 400g of tantalum powder in the nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.3m 3 /h, pass nitrogen gas at room temperature for 1 hour to discharge the air, then raise the temperature to 900°C, and treat the tantalum in a nitrogen atmosphere. Nitriding the powder for 15 minutes; the mass purity of the tantalum powder is not less than 99.5%, and the particle size of the tantalum powder is not less than 200 mesh;

步骤二、将步骤一中经渗氮处理后的钽粉末置于等离子烧结炉中,调节压强为300MPa,在950℃条件下将经渗氮处理后的钽粉末烧结处理5min,得到钽基合金。Step 2. Place the tantalum powder after nitriding treatment in step 1 in a plasma sintering furnace, adjust the pressure to 300 MPa, and sinter the tantalum powder after nitriding treatment at 950° C. for 5 minutes to obtain a tantalum-based alloy.

对比例2制备的钽基合金中氮含量为0.15%。The nitrogen content in the tantalum-based alloy prepared in Comparative Example 2 was 0.15%.

图4为对比例2制备的钽基合金的硬度梯度趋势图,从图4可以看出,经过渗氮处理和烧结处理两步工艺制备的钽基合金内部也具有比较明显的硬度梯度结构,随着距表面距离的增加,钽基合金的微观硬度逐渐减小,从表层的6.0GPa逐渐下降到距表面距离25μm处的4.8GPa,再下降到芯部的3.0GPa。结合图3和图4可以看出,采用氧氮共渗处理工艺制备的钽基合金具有更加明显的硬度梯度结构和更高的整体微观硬度。Fig. 4 is the hardness gradient trend graph of the tantalum-based alloy prepared in Comparative Example 2. It can be seen from Fig. 4 that the tantalum-based alloy prepared by the two-step process of nitriding and sintering also has a relatively obvious hardness gradient structure inside. As the distance from the surface increases, the microhardness of the tantalum-based alloy gradually decreases, from 6.0GPa at the surface to 4.8GPa at a distance of 25μm from the surface, and then to 3.0GPa at the core. Combining Figures 3 and 4, it can be seen that the tantalum-based alloy prepared by the oxynitriding process has a more obvious hardness gradient structure and a higher overall microhardness.

对比例2中制备的钽基合金的室温力学性能测试结果为:断裂延伸率为19%,屈服强度为1100MPa,断裂强度为1150MPa。The test results of the mechanical properties of the tantalum-based alloy prepared in Comparative Example 2 at room temperature are: the elongation at break is 19%, the yield strength is 1100 MPa, and the breaking strength is 1150 MPa.

结合上述对比例1和对比例2制备的钽基合金的氮含量和硬度梯度趋势图,可以说明在采用氧氮共渗处理的工艺中由于氧的催渗作用促进了氮原子在钽中的渗入,使渗层固溶的氮及形成的氮化物增加,从而增大钽中氧氮共渗的化合物层和扩散层的深度,更加有利于提高钽基合金材料的硬度及进一步改善材料的综合力学性能。Combining the nitrogen content and hardness gradient trend graphs of the tantalum-based alloys prepared in Comparative Example 1 and Comparative Example 2 above, it can be shown that the infiltration of nitrogen atoms in tantalum is promoted by the infiltration of oxygen in the process of oxynitridation treatment. , so that the nitrogen in solid solution and the nitride formed in the permeation layer increase, thereby increasing the depth of the compound layer and the diffusion layer of oxynitride in tantalum, which is more conducive to improving the hardness of the tantalum-based alloy material and further improving the comprehensive mechanics of the material performance.

结合图1和图2可看出,在经过真空退火处理后,钽基合金的硬度梯度结构仍然存在;结合对比例1和对比例2中制备的钽基合金的室温力学性能测试结果可以进一步看出,采用氧氮共渗处理工艺能够制备得到综合力学性能更好的钽基合金材料;结合实施例1和对比例1中制备的钽基合金的综合力学性能可看出,经过真空退火处理的钽基合金在保留材料塑性的同时,能够明显提高材料的硬度,使钽基合金具有更好的综合力学性能。Combining Figures 1 and 2, it can be seen that after vacuum annealing, the hardness gradient structure of the tantalum-based alloy still exists; combined with the room temperature mechanical properties of the tantalum-based alloys prepared in Comparative Example 1 and Comparative Example 2, the test results can be further seen It can be seen that the tantalum-based alloy material with better comprehensive mechanical properties can be prepared by using the oxygen-nitriding treatment process; combined with the comprehensive mechanical properties of the tantalum-based alloy prepared in Example 1 and Comparative Example 1, it can be seen that the vacuum annealed The tantalum-based alloy can significantly increase the hardness of the material while retaining the plasticity of the material, so that the tantalum-based alloy has better comprehensive mechanical properties.

本实施例制备的钽基合金内部具有明显的氧氮含量浓度梯度和硬度梯度结构,使材料在具有较高强度的同时,还保留了较好的塑性,实现了钽基合金的强度与塑性的良好配合。The tantalum-based alloy prepared in this example has obvious oxygen and nitrogen content concentration gradient and hardness gradient structure inside, so that the material retains good plasticity while having high strength, and realizes the balance between the strength and plasticity of the tantalum-based alloy. Good fit.

实施例2Example 2

本实施例包括以下步骤:This embodiment includes the following steps:

步骤一、将400g钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.12m3/h,氧气流量为0.08m3/h,在800℃条件下对钽粉末进行氧氮共渗处理30min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目,所述氧氮共渗处理过程中控制渗氮炉中氧的体积含量不低于5%;Step 1. Put 400g of tantalum powder in the nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.12m 3 /h, and the oxygen flow rate to 0.08m 3 /h, and carry out oxynitridation on the tantalum powder at 800°C Treat for 30 minutes; the mass purity of the tantalum powder is not less than 99.5%, the particle size of the tantalum powder is not less than 200 mesh, and the volume content of oxygen in the nitriding furnace is controlled to be not less than 5% during the oxynitriding process;

步骤二、将步骤一中经氧氮共渗处理后的钽粉末置于等离子烧结炉中,调节压强为200MPa,在1000℃条件下将经氧氮共渗处理后的钽粉末烧结处理3min,得到钽基合金;Step 2. Put the tantalum powder treated by oxynitriding in step 1 in a plasma sintering furnace, adjust the pressure to 200MPa, and sinter the tantalum powder treated by oxynitriding at 1000°C for 3 minutes to obtain Tantalum-based alloys;

步骤三、将步骤二中所述钽基合金置于真空退火炉中,调节真空度为10-1Pa,在800℃条件下将钽基合金真空退火处理2h。Step 3. Put the tantalum-based alloy described in step 2 in a vacuum annealing furnace, adjust the vacuum degree to 10 −1 Pa, and vacuum anneal the tantalum-based alloy at 800° C. for 2 hours.

图5为实施例2制备的钽基合金的硬度压痕形貌图,实施例2中制备的钽基合金的室温力学性能测试结果为:断裂延伸率为15%,具有较好的塑性,屈服强度为1250MPa(该实施例制备的钽基合金的屈服强度是纯钽粉末冶金材料屈服强度的3.29倍)。Figure 5 is the hardness indentation topography of the tantalum-based alloy prepared in Example 2. The room temperature mechanical properties test results of the tantalum-based alloy prepared in Example 2 are: the elongation at break is 15%, and it has good plasticity and yield The strength is 1250MPa (the yield strength of the tantalum-based alloy prepared in this example is 3.29 times that of the pure tantalum powder metallurgy material).

对比例3Comparative example 3

对比例3与实施例2相同,其不同之处在于:不对步骤二中所述钽基合金进行真空退火处理。Comparative Example 3 is the same as Example 2, except that the tantalum-based alloy in Step 2 is not subjected to vacuum annealing.

对比例3制备的钽基合金中的氧含量为0.06%,氮含量为0.08%,钽基合金的相对密度为99%。The oxygen content in the tantalum-based alloy prepared in Comparative Example 3 was 0.06%, the nitrogen content was 0.08%, and the relative density of the tantalum-based alloy was 99%.

图6为对比例3制备的钽基合金的硬度压痕形貌图,图7为对比例3制备的钽基合金的硬度梯度趋势图,结合图6和图7可以看出,经过氧氮共渗处理和烧结处理两步工艺制备的钽基合金内部具有明显的硬度梯度结构,随着距表面距离的增加,钽基合金的微观硬度逐渐减小,从表层的4.1GPa逐渐下降到距表面距离25μm处的3.6GPa,再下降到芯部的2.9GPa。Fig. 6 is the hardness indentation topography diagram of the tantalum-based alloy prepared in comparative example 3, and Fig. 7 is the hardness gradient trend diagram of the tantalum-based alloy prepared in comparative example 3. Combining Fig. 6 and Fig. 7, it can be seen that after oxygen-nitrogen co- The tantalum-based alloy prepared by the two-step process of infiltration treatment and sintering treatment has an obvious hardness gradient structure inside. As the distance from the surface increases, the microhardness of the tantalum-based alloy gradually decreases, from 4.1GPa on the surface to the distance from the surface. 3.6GPa at 25μm, and then down to 2.9GPa at the core.

对比例3中制备的钽基合金的室温力学性能测试结果为:断裂延伸率为22%,屈服强度为1080MPa,断裂强度为1120MPa。The test results of the mechanical properties of the tantalum-based alloy prepared in Comparative Example 3 at room temperature are: the elongation at break is 22%, the yield strength is 1080 MPa, and the breaking strength is 1120 MPa.

对比例4Comparative example 4

本对比例包括以下步骤:This comparative example includes the following steps:

步骤一、将400g钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.3m3/h,常温下通入氮气1h以排出空气,然后升温至800℃,在氮气气氛下对钽粉末进行渗氮处理30min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目;Step 1. Put 400g of tantalum powder in the nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.3m 3 /h, pass nitrogen gas at room temperature for 1 hour to discharge the air, then raise the temperature to 800°C, and treat the tantalum in a nitrogen atmosphere. Nitriding the powder for 30 minutes; the mass purity of the tantalum powder is not less than 99.5%, and the particle size of the tantalum powder is not less than 200 mesh;

步骤二、将步骤一中经渗氮处理后的钽粉末置于等离子烧结炉中,调节压强为200MPa,在1000℃条件下将经渗氮处理后的钽粉末烧结处理3min,得到钽基合金。Step 2. Place the tantalum powder after nitriding treatment in step 1 in a plasma sintering furnace, adjust the pressure to 200 MPa, and sinter the tantalum powder after nitriding treatment at 1000° C. for 3 minutes to obtain a tantalum-based alloy.

对比例4制备的钽基合金中氮含量为0.07%。The nitrogen content in the tantalum-based alloy prepared in Comparative Example 4 was 0.07%.

图8为对比例4制备的钽基合金的硬度梯度趋势图,从图8可以看出,经过渗氮处理和烧结处理两步工艺制备的钽基合金内部也具有比较明显的硬度梯度结构,随着距表面距离的增加,钽基合金的微观硬度逐渐减小,从表层的3.6GPa逐渐下降到距表面距离25μm处的3.2GPa,再下降到芯部的2.8GPa。结合图7和图8可以看出,采用氧氮共渗处理工艺制备的钽基合金具有更加明显的硬度梯度结构和更高的整体微观硬度。Fig. 8 is the hardness gradient trend graph of the tantalum-based alloy prepared in Comparative Example 4. It can be seen from Fig. 8 that the tantalum-based alloy prepared by the two-step process of nitriding and sintering also has a relatively obvious hardness gradient structure inside. As the distance from the surface increases, the microhardness of the tantalum-based alloy gradually decreases, from 3.6GPa at the surface to 3.2GPa at a distance of 25μm from the surface, and then to 2.8GPa at the core. Combining Figures 7 and 8, it can be seen that the tantalum-based alloy prepared by the oxynitriding process has a more obvious hardness gradient structure and a higher overall microhardness.

对比例4中制备的钽基合金的室温力学性能测试结果为:断裂延伸率为23%,屈服强度为980MPa,断裂强度为1010MPa。The test results of the mechanical properties of the tantalum-based alloy prepared in Comparative Example 4 at room temperature are: the elongation at break is 23%, the yield strength is 980 MPa, and the breaking strength is 1010 MPa.

结合上述对比例3和对比例4制备的钽基合金的氮含量和硬度梯度趋势图,可以说明在采用氧氮共渗处理的工艺中由于氧的催渗作用促进了氮原子在钽中的渗入,使渗层固溶的氮及形成的氮化物增加,从而增大钽中氧氮共渗的化合物层和扩散层的深度,更加有利于提高钽基合金材料的硬度及进一步改善材料的综合力学性能。Combining the nitrogen content and hardness gradient trend graphs of the tantalum-based alloys prepared in Comparative Example 3 and Comparative Example 4 above, it can be explained that the infiltration of nitrogen atoms in tantalum is promoted by the infiltration of oxygen in the process of oxynitridation treatment. , so that the nitrogen in solid solution and the nitride formed in the permeation layer increase, thereby increasing the depth of the compound layer and the diffusion layer of oxynitride in tantalum, which is more conducive to improving the hardness of the tantalum-based alloy material and further improving the comprehensive mechanics of the material performance.

结合图5和图6可看出,在经过真空退火处理后,钽基合金的硬度梯度结构仍然存在;结合对比例3和对比例4中制备的钽基合金的室温力学性能测试结果可以进一步看出,采用氧氮共渗处理工艺能够制备得到综合力学性能更好的钽基合金材料;结合实施例2和对比例3中制备的钽基合金的综合力学性能可看出,经过真空退火处理的钽基合金在保留材料塑性的同时,能够明显提高材料的硬度,使钽基合金具有更好的综合力学性能。Combining Figures 5 and 6, it can be seen that after vacuum annealing, the hardness gradient structure of the tantalum-based alloy still exists; combined with the test results of the room temperature mechanical properties of the tantalum-based alloys prepared in Comparative Example 3 and Comparative Example 4, it can be further seen It can be seen that the tantalum-based alloy material with better comprehensive mechanical properties can be prepared by using the oxygen-nitriding treatment process; combined with the comprehensive mechanical properties of the tantalum-based alloy prepared in Example 2 and Comparative Example 3, it can be seen that the vacuum annealed The tantalum-based alloy can significantly increase the hardness of the material while retaining the plasticity of the material, so that the tantalum-based alloy has better comprehensive mechanical properties.

本实施例制备的钽基合金内部具有明显的氧氮含量浓度梯度和硬度梯度结构,使材料在具有较高强度的同时,还保留了较好的塑性,实现了钽基合金的强度与塑性的良好配合。The tantalum-based alloy prepared in this example has obvious oxygen and nitrogen content concentration gradient and hardness gradient structure inside, so that the material retains good plasticity while having high strength, and realizes the balance between the strength and plasticity of the tantalum-based alloy. Good fit.

实施例3Example 3

步骤一、将400g钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.08m3/h,在1000℃条件下对钽粉末进行氧氮共渗处理5min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目,所述氧氮共渗处理过程中控制渗氮炉中氧的体积含量不低于5%;Step 1. Put 400g of tantalum powder in a nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.08m 3 /h, and carry out oxynitriding treatment on the tantalum powder at 1000°C for 5 minutes; the mass of the tantalum powder The purity is not less than 99.5%, the particle size of the tantalum powder is not less than 200 mesh, and the volume content of oxygen in the nitriding furnace is controlled to be not less than 5% during the oxynitriding process;

步骤二、将步骤一中经氧氮共渗处理后的钽粉末置于等离子烧结炉中,调节压强为400MPa,在900℃条件下将经氧氮共渗处理后的钽粉末烧结处理10min,得到钽基合金;Step 2. Put the tantalum powder treated by oxynitriding in step 1 in a plasma sintering furnace, adjust the pressure to 400MPa, and sinter the tantalum powder treated by oxynitriding at 900°C for 10 minutes to obtain Tantalum-based alloys;

步骤三、将步骤二中所述钽基合金置于真空退火炉中,调节真空度为10-3Pa,在1000℃条件下将钽基合金真空退火处理0.5h。Step 3. Put the tantalum-based alloy described in step 2 in a vacuum annealing furnace, adjust the vacuum degree to 10 −3 Pa, and vacuum anneal the tantalum-based alloy at 1000° C. for 0.5 h.

本实施例制备的钽基合金随着距表面距离的增加,钽基合金的微观硬度逐渐减小,具有明显的硬度梯度。测量钽基合金的室温力学性能结果为:延伸率约为13%,屈服强度为1310MPa,说明钽基合金在硬度提高的同时保留较好的塑性。As the distance from the surface of the tantalum-based alloy prepared in this example increases, the microhardness of the tantalum-based alloy gradually decreases, and there is an obvious hardness gradient. The results of measuring the mechanical properties of the tantalum-based alloy at room temperature are: the elongation is about 13%, and the yield strength is 1310MPa, indicating that the tantalum-based alloy retains good plasticity while increasing the hardness.

本实施例制备的钽基合金内部具有明显的氧氮含量浓度梯度和硬度梯度结构,使材料在具有较高强度的同时,还保留了较好的塑性,实现了钽基合金的强度与塑性的良好配合。The tantalum-based alloy prepared in this example has obvious oxygen and nitrogen content concentration gradient and hardness gradient structure inside, so that the material retains good plasticity while having high strength, and realizes the balance between the strength and plasticity of the tantalum-based alloy. Good fit.

实施例4Example 4

步骤一、将400g钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.2m3/h,氧气流量为0.15m3/h,在600℃条件下对钽粉末进行氧氮共渗处理90min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目,所述氧氮共渗处理过程中控制渗氮炉中氧的体积含量不低于5%;Step 1. Put 400g of tantalum powder in the nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.2m 3 /h, and the oxygen flow rate to 0.15m 3 /h, and carry out oxynitridation of the tantalum powder at 600°C Treat for 90 minutes; the mass purity of the tantalum powder is not less than 99.5%, the particle size of the tantalum powder is not less than 200 mesh, and the volume content of oxygen in the nitriding furnace is controlled to be not less than 5% during the oxynitriding process;

步骤二、将步骤一中经氧氮共渗处理后的钽粉末置于等离子烧结炉中,调节压强为500MPa,在1100℃条件下将经氧氮共渗处理后的钽粉末烧结处理1min,得到钽基合金;Step 2. Put the tantalum powder treated by oxynitriding in step 1 in a plasma sintering furnace, adjust the pressure to 500MPa, and sinter the tantalum powder treated by oxynitriding at 1100°C for 1 min to obtain Tantalum-based alloys;

步骤三、将步骤二中所述钽基合金置于真空退火炉中,调节真空度为10-4Pa,在700℃条件下将钽基合金真空退火处理5h。Step 3. Put the tantalum-based alloy described in step 2 in a vacuum annealing furnace, adjust the vacuum degree to 10 −4 Pa, and vacuum anneal the tantalum-based alloy at 700° C. for 5 hours.

本实施例制备的钽基合金随着距表面距离的增加,钽基合金的微观硬度逐渐减小,具有明显的硬度梯度。测量钽基合金的室温力学性能结果为:延伸率约为14%,屈服强度为1260MPa,说明钽基合金在硬度提高的同时保留较好的塑性。As the distance from the surface of the tantalum-based alloy prepared in this example increases, the microhardness of the tantalum-based alloy gradually decreases, and there is an obvious hardness gradient. The results of measuring the mechanical properties of the tantalum-based alloy at room temperature are: the elongation is about 14%, and the yield strength is 1260MPa, indicating that the tantalum-based alloy retains good plasticity while increasing the hardness.

本实施例制备的钽基合金内部具有明显的氧氮含量浓度梯度和硬度梯度结构,使材料在具有较高强度的同时,还保留了较好的塑性,实现了钽基合金的强度与塑性的良好配合。The tantalum-based alloy prepared in this example has obvious oxygen and nitrogen content concentration gradient and hardness gradient structure inside, so that the material retains good plasticity while having high strength, and realizes the balance between the strength and plasticity of the tantalum-based alloy. Good fit.

实施例5Example 5

步骤一、将400g钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.05m3/h,在900℃条件下对钽粉末进行氧氮共渗处理10min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目,所述氧氮共渗处理过程中控制渗氮炉中氧的体积含量不低于5%;Step 1. Place 400g of tantalum powder in a nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.05m 3 /h, and carry out oxynitridation treatment on the tantalum powder at 900°C for 10 minutes; the mass of the tantalum powder The purity is not less than 99.5%, the particle size of the tantalum powder is not less than 200 mesh, and the volume content of oxygen in the nitriding furnace is controlled to be not less than 5% during the oxynitriding process;

步骤二、将步骤一中经氧氮共渗处理后的钽粉末置于等离子烧结炉中,调节压强为250MPa,在800℃条件下将经氧氮共渗处理后的钽粉末烧结处理30min,得到钽基合金;Step 2. Put the tantalum powder treated by oxynitriding in step 1 in a plasma sintering furnace, adjust the pressure to 250MPa, and sinter the tantalum powder treated by oxynitriding at 800°C for 30 minutes to obtain Tantalum-based alloys;

步骤三、将步骤二中所述钽基合金置于真空退火炉中,调节真空度为10-2Pa,在1050℃条件下将钽基合金真空退火处理0.5h。Step 3. Put the tantalum-based alloy described in step 2 in a vacuum annealing furnace, adjust the vacuum degree to 10 −2 Pa, and vacuum anneal the tantalum-based alloy at 1050° C. for 0.5 h.

本实施例制备的钽基合金随着距表面距离的增加,钽基合金的微观硬度逐渐减小,具有明显的硬度梯度。测量钽基合金的室温力学性能结果为:延伸率约为13.5%,屈服强度为1300MPa,说明钽基合金在硬度提高的同时保留较好的塑性。As the distance from the surface of the tantalum-based alloy prepared in this example increases, the microhardness of the tantalum-based alloy gradually decreases, and there is an obvious hardness gradient. The results of measuring the mechanical properties of the tantalum-based alloy at room temperature are: the elongation is about 13.5%, and the yield strength is 1300MPa, indicating that the tantalum-based alloy retains good plasticity while increasing the hardness.

本实施例制备的钽基合金内部具有明显的氧氮含量浓度梯度和硬度梯度结构,使材料在具有较高强度的同时,还保留了较好的塑性,实现了钽基合金的强度与塑性的良好配合。The tantalum-based alloy prepared in this example has obvious oxygen and nitrogen content concentration gradient and hardness gradient structure inside, so that the material retains good plasticity while having high strength, and realizes the balance between the strength and plasticity of the tantalum-based alloy. Good fit.

实施例6Example 6

步骤一、将400g钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.12m3/h,在800℃条件下对钽粉末进行氧氮共渗处理40min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目,所述氧氮共渗处理过程中控制渗氮炉中氧的体积含量不低于5%;Step 1. Place 400g of tantalum powder in a nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.12m 3 /h, and carry out oxynitriding treatment on the tantalum powder at 800°C for 40 minutes; the mass of the tantalum powder The purity is not less than 99.5%, the particle size of the tantalum powder is not less than 200 mesh, and the volume content of oxygen in the nitriding furnace is controlled to be not less than 5% during the oxynitriding process;

步骤二、将步骤一中所述经氧氮共渗处理后的钽粉末置于等离子烧结炉中,调节压强为350MPa,在950℃条件下将经氧氮共渗处理后的钽粉末烧结处理16min,得到钽基合金;Step 2. Place the tantalum powder after oxynitriding treatment in step 1 in a plasma sintering furnace, adjust the pressure to 350MPa, and sinter the tantalum powder after oxynitriding treatment at 950°C for 16 minutes , to obtain a tantalum-based alloy;

步骤三、将步骤二中所述钽基合金置于真空退火炉中,调节真空度为10-2Pa,在860℃条件下将钽基合金真空退火处理2.5h。Step 3. Put the tantalum-based alloy described in step 2 in a vacuum annealing furnace, adjust the vacuum degree to 10 −2 Pa, and vacuum anneal the tantalum-based alloy at 860° C. for 2.5 hours.

本实施例制备的钽基合金随着距表面距离的增加,钽基合金的微观硬度逐渐减小,具有明显的硬度梯度。测量钽基合金的室温力学性能结果为:延伸率约为12%,屈服强度为1350MPa,说明钽基合金在硬度提高的同时保留较好的塑性。As the distance from the surface of the tantalum-based alloy prepared in this example increases, the microhardness of the tantalum-based alloy gradually decreases, and there is an obvious hardness gradient. The results of measuring the mechanical properties of the tantalum-based alloy at room temperature are: the elongation is about 12%, and the yield strength is 1350MPa, indicating that the tantalum-based alloy retains good plasticity while increasing the hardness.

本实施例制备的钽基合金内部具有明显的氧氮含量浓度梯度和硬度梯度结构,使材料在具有较高强度的同时,还保留了较好的塑性,实现了钽基合金的强度与塑性的良好配合。The tantalum-based alloy prepared in this example has obvious oxygen and nitrogen content concentration gradient and hardness gradient structure inside, so that the material retains good plasticity while having high strength, and realizes the balance between the strength and plasticity of the tantalum-based alloy. Good fit.

以上所述,仅是本发明的较佳实施例,并非对本发明作任何限制,凡是根据本发明技术实质对以上实施例所作的任何简单修改、变更以及等效结构变化,均仍属于本发明技术方案的保护范围内。The above are only preferred embodiments of the present invention, and do not limit the present invention in any way. All simple modifications, changes and equivalent structural changes made to the above embodiments according to the technical essence of the present invention still belong to the technical aspects of the present invention. within the scope of protection of the scheme.

Claims (7)

1.一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,该方法包括以下步骤:1. A method for preparing a tantalum-based alloy with a gradient structure through solid solution strengthening, characterized in that the method may further comprise the steps: 步骤一、将钽粉末置于渗氮炉中,调节渗氮炉的氮气流量为0.05m3/h~0.2m3/h,在600℃~1000℃条件下对钽粉末进行氧氮共渗处理5min~90min;所述钽粉末的质量纯度不小于99.5%,所述钽粉末的粒度不小于200目,所述氧氮共渗处理过程中控制渗氮炉中氧的体积含量不低于5%;Step 1. Put the tantalum powder in the nitriding furnace, adjust the nitrogen flow rate of the nitriding furnace to 0.05m 3 /h~0.2m 3 /h, and carry out oxynitriding treatment on the tantalum powder under the condition of 600℃~1000℃ 5min to 90min; the mass purity of the tantalum powder is not less than 99.5%, the particle size of the tantalum powder is not less than 200 mesh, and the volume content of oxygen in the nitriding furnace is controlled to be not less than 5% during the oxynitriding process ; 步骤二、将步骤一中经氧氮共渗处理后的钽粉末置于等离子烧结炉中,调节等离子烧结炉的压强为200MPa~500MPa,在800℃~1100℃条件下将经氧氮共渗处理后的钽粉末烧结处理1min~30min,得到钽基合金;Step 2. Put the tantalum powder treated by oxynitriding in step 1 in a plasma sintering furnace, adjust the pressure of the plasma sintering furnace to 200MPa-500MPa, and place the tantalum powder treated by oxynitriding in step 1 at 800°C-1100°C. The final tantalum powder is sintered for 1 to 30 minutes to obtain a tantalum-based alloy; 步骤三、将步骤二中所述钽基合金置于真空退火炉中,调节真空退火炉的真空度为10-4Pa~10-1Pa,在700℃~1050℃条件下将钽基合金真空退火处理0.5h~5h。Step 3. Place the tantalum-based alloy described in step 2 in a vacuum annealing furnace, adjust the vacuum degree of the vacuum annealing furnace to 10 -4 Pa to 10 -1 Pa, and vacuum the tantalum-based alloy at 700°C to 1050°C Annealing treatment 0.5h ~ 5h. 2.按照权利要求1所述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,步骤一中所述氮气流量为0.08m3/h~0.12m3/h,氧氮共渗处理的温度为800℃~1000℃,氧氮共渗处理的时间为5min~30min。2. A method for preparing a tantalum-based alloy with a gradient structure according to claim 1, wherein the flow rate of nitrogen gas in step 1 is 0.08m 3 /h to 0.12m 3 / h, oxygen The temperature of nitriding treatment is 800° C. to 1000° C., and the time of oxynitriding treatment is 5 minutes to 30 minutes. 3.按照权利要求2所述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,所述氮气流量为0.1m3/h,氧氮共渗处理的温度为900℃,氧氮共渗处理的时间为15min。3. A method for preparing a tantalum-based alloy with a gradient structure according to claim 2, wherein the flow rate of the nitrogen gas is 0.1 m 3 /h, and the temperature of the oxynitriding treatment is 900° C. , The time of oxynitriding treatment is 15min. 4.按照权利要求1所述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,步骤二中所述压强为200MPa~400MPa,烧结处理的温度为900℃~1000℃,烧结处理的时间为3min~10min。4. A method for preparing a tantalum-based alloy with a gradient structure according to claim 1, characterized in that the pressure in step 2 is 200MPa-400MPa, and the sintering temperature is 900°C-1000°C , the time of sintering treatment is 3min~10min. 5.按照权利要求4所述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,所述压强为300MPa,烧结处理的温度为950℃,烧结处理的时间为5min。5. A method for preparing a tantalum-based alloy with a gradient structure according to claim 4, wherein the pressure is 300 MPa, the sintering temperature is 950° C., and the sintering time is 5 minutes. 6.按照权利要求1所述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,步骤三中所述真空度为10-3Pa~10-1Pa,真空退火处理的温度为800℃~1000℃,真空退火处理的时间为0.5h~2h。6. A method for preparing a tantalum-based alloy with a gradient structure according to claim 1, wherein the degree of vacuum in step 3 is 10 -3 Pa to 10 -1 Pa, and the vacuum annealing treatment The temperature is 800°C to 1000°C, and the time for vacuum annealing is 0.5h to 2h. 7.按照权利要求6所述的一种固溶强化制备具有梯度结构的钽基合金的方法,其特征在于,所述真空度为10-2Pa,真空退火处理的温度为900℃,真空退火处理的时间为1h。7. A method for preparing a tantalum-based alloy with a gradient structure according to claim 6, wherein the degree of vacuum is 10 -2 Pa, the temperature of the vacuum annealing treatment is 900°C, and the vacuum annealing The processing time is 1h.
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